Forming fibre-plastics composites

• US 4,657,717 A
• Filed: 03/15/1985
• Issued: 04/14/1987
• Est. Priority Date: 03/16/1984
• Status: Expired due to Term

• Current Assignee: Alcan Incorporated (Alcan)
• Original Assignee: Alcan Incorporated (Alcan)
• Inventors: Cattanach, James B., Barnes, Anthony J.
• Primary Examiner(s): Lowe, James
• Application Number:
  US06/712,009
• Time in Patent Office: 760 Days
• Field of Search: 264/316, 264/257, 264/275, 264/1.9, 264/102, 264/258, 264/292, 264/314, 264/324, 249/94
• US Class Current: 264/102
• CPC Class Codes: B29C 2043/3644 Vacuum bags; Details thereof, e.g. fixing or clamping
• CPC Class Codes: B29C 43/12 using bags surrounding the moulding material or using membranes contacting the moulding material
• CPC Class Codes: B29C 43/3642 Bags, bleeder sheets or cauls for isostatic pressing
• CPC Class Codes: B29C 51/28 for applying pressure through the wall of an inflated bag or diaphragm
• CPC Class Codes: B29C 70/42 for producing articles of definite length, i.e. discrete articles
• CPC Class Codes: B29C 70/542 Placing or positioning the reinforcement in a covering or packaging element before or during moulding, e.g. drawing in a sleeve
• CPC Class Codes: B29K 2105/06 containing reinforcements, fillers or inserts
• CPC Class Codes: B29K 2705/00 Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
• CPC Class Codes: B29L 2009/00 Layered products
• CPC Class Codes: B32B 15/08 of synthetic resin
• CPC Class Codes: B32B 2305/076 Prepregs
• CPC Class Codes: B32B 2309/68 Vacuum
• CPC Class Codes: B32B 3/28 characterised by a layer comprising a deformed thin sheet , i.e. the layer having its entire thickness deformed out of the plane, e.g. corrugated, crumpled B32B29/08 takes precedence
• CPC Class Codes: B32B 7/12 using interposed adhesives or interposed materials with bonding properties

Abstract

A plastics composite of fibres in a thermoformable matrix is formed by contacting the composite with a sheet of metal and deforming the metal plastically. The thermoformable matrix may be thermoplastic or thermosetting and the metal may be superplastic. The matrix may be deformed between the sheet and another sheet or between the sheet and a mould. Thin bodies of complex shape may be formed.

Claims

1. A method of forming a three dimensional shaped article of a plastics composite comprising superimposed layers of fibers dispersed in a matrix of a thermoformable material, comprising the steps of

providing a body of said composite to be reshaped and having a first side and a second side;

contacting at least the first side of said body of said composite with a sheet of a metal which is capable of being plastically deformed at an elevated temperature,

clamping edges of said metal sheet to prevent movement of said edges during subsequent deformation, and applying vacuum to remove air from between said metal sheet and said body to bring the composite body tightly against the metal sheet and to provide support for said body;

bringing the metal sheet and the composite body to an elevated temperature at which the metal sheet can be substantially plastically deformed and at which the composite body can conform to the plastically deformed shape of the metal sheet, and

applying fluid pressure to the metal sheet while the second side of the composite body is at least partly reshaped by a mold so that the metal sheet becomes substantially plastically deformed to a relatively new deep shaped geometry and the first side of the composite body is formed to the relatively deep shaped new geometry by the plastic deformation of the metal sheet, including relative movement of the fibers of the superimposed layers to accommodate themselves to the new geometry without buckling, the shape of the plastics composite thereby obtained being defined on at least said first side by the plastic flow of the metal sheet.

2. A method according to claim 1, in which the thermoformable material is thermoplastic.

3. A method according to claim 1, in which the thermoformable material is thermosettable.

4. A method according to claim 1, in which the body of composite comprises a sheet of thickness from 0.25 mm to 25 mm.

5. A method according to claim 1, in which the body of composite comprises a pre-formed consolidated plastics sheet containing said superimposed layers of fibres and the composite sheet is curved about at least one axis in the plane of the composite sheet when the metal sheet is urged against the body.

6. A method according to claim 1, in which the body of composite comprises an assembly of prepreg sheets and the prepreg sheets are consolidated together when the metal sheet is urged against the body.

7. A method according to claim 1, in which the metal sheet is superplastic.

8. A method according to claim 1, in which the body comprises a plurality of separate pieces of said composite and the pieces are joined together when the sheet is urged against the body.

9. A method according to claim 1, in which the metal sheet comprises an inflatable diaphragm or parison.

10. A method according to claim 1, in which the body is positioned directly between the metal sheet and a surface of said mould and the metal sheet is deformed when urged against the body to press the body against the mould surface.

11. A method according to claim 10, in which the mould surface is provided with apertures, members to be attached to the body are placed in the apertures and the members become attached to the body when the body is pressed against the mould surface.

12. A method according to claim 1, in which the metal sheet has at least one upstanding portion extending into or around the body when the sheet is urged against the body, said upstanding portion defining an edge of the shaped article extending in the direction transverse to the sheet.

13. A method according to claim 12, in which the body is positioned between said metal sheet and another deformable sheet which has an aperture opposite said upstanding portion, the upstanding portion entering the aperture when said metal sheet is urged against the body.

14. A method according to claim 1, in which a lubricant is applied between the surface of the metal sheet and the body.

15. A method according to claim 1, in which a layer of material is interposed between the metal sheet and the body and said material becomes adhered to the shaped article on urging of the sheet against the body.

16. A method according to claim 1, in which an adhesive is applied between the surface of the metal sheet and the body and the sheet is adhered to the body when urged against the body.

17. A method according to claim 1, in which at least one member to be attached to the body is positioned in contact with the body and becomes attached to the body on plastic deformation of the sheet to shape the body.

18. A method of forming a shaped article of a plastics composite comprising fibers dispersed in a matrix of a thermoformable material, comprising the steps of

providing a body of said composite to be reshaped and having a first side and a second side;

confining both said first and second sides of said body of said composite between sheets of metal which are capable of being plastically deformed at an elevated temperature;

restraining the edges of said metal sheets;

bringing said metal sheets and the body to an elevated temperature at which the metal sheets can be plastically deformed and at which the body can conform to the shape of the metal sheets;

applying fluid pressure to one of the metal sheets at such a pressure so that the metal sheets are plastically stretched relative to the restrained edges and the body is formed to shape between the stretched metal sheets, the shape of the plastics composite thereby obtained being defined by the plastic flow of the metal sheets; and

separating the stretched metal sheets from the resultant shaped article.

19. A method according to claim 18, in which one of said sheet is perforate to allow gases trapped between the sheets to escape.

20. A method according to claim 18, in which the space between said metal sheets is evacuated to remove gases between the sheets.

21. A method according to claim 20, in which the peripheries of the sheets are joined by a rigid gas-tight frame to form an enclosure surrounding the body, the frame having an aperture and means for creating a vacuum in the enclosure are connected to the aperture, a vacuum is established in the enclosure and said metal sheet is urged against the body while the vacuum is maintained in the enclosure.

22. A method according to claim 21, in which after deformation of the sheets and body the vacuum in the enclosure is maintained while the body is allowed to cool.